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Green Airplanes 02−10−1
EMS CDU Switch Control Page Settings 02−10−3
Green Airplanes 9005 and Subsequent 02−10−3
LIST OF ILLUSTRATIONS
CENTRE OF GRAVITY
Figure 02−03−1 Centre of Gravity (CG) Envelope 02−03−2
OPERATING LIMITATIONS
Figure 02−04−1 Altitude and Temperature Operating Limit 02−04−2
POWER PLANT
Figure 02−05−1 Engine Air Start Envelope 02−05−3
Figure 02−05−2 Engine Oil Pressure Limits 02−05−8
OPERATING SPEEDS
Figure 02−06−1 Maximum Operating Speed and Mach Number 02−06−1
Figure 02−06−2 Design Maneuvering Speeds 02−06−3
LIMITATIONS
TABLE OF CONTENTS
Flight Crew Operating Manual REV 13, Nov 10, 2006
CSP 700−5000−6
Volume 1
02−00−4
Page
1. INTRODUCTION
A. General
The limitations included in this chapter contain items peculiar to the GLOBAL 5000® airplane.
Observance of these limitations is mandatory.
B. Kinds of Airplane Operation
The airplane is certified for day and night operations, in the following conditions when the
equipment and instruments required by the airworthiness and operating regulations are
approved, installed and in an operable condition:
• VFR and IFR
The airplane is certified for ditching when the safety equipment specified by the applicable
regulations is installed.
The airplane is certified for flight in icing conditions.
The airplane is not to be used for transportation of passengers or cargo unless it has been
completed by the installation of an approved interior.
LIMITATIONS
INTRODUCTION
REV 7, Dec 01, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−01−1
LIMITATIONS
INTRODUCTION
Flight Crew Operating Manual Mar 12, 2004
CSP 700−5000−6
Volume 1
02−01−2
THIS PAGE INTENTIONALLY LEFT BLANK
1. STRUCTURAL WEIGHT
A. Structural Weight Limitations
Maximum taxi and ramp weight: 39,893 kg (87,950 lb)
Maximum take-off weight: 39,780 kg (87,700 lb)
Maximum landing weight: 35,652 kg (78,600 lb)
Maximum zero fuel weight: 25,401 kg (56,000 lb)
Minimum flight weight: 23,224 kg (51,200 lb)
Minimum operating empty weight: 21,772 kg (48,000 lb)
Aircraft incorporating 40,687 kg (89,700 lb) MTOW placard
Maximum taxi and ramp weight: 40,801 kg (89,950 lb)
Maximum take-off weight: 40,687 kg (89,700 lb)
Maximum landing weight: 35,652 kg (78,600 lb)
Maximum zero fuel weight: 25,401 kg (56,000 lb)
Minimum flight weight: 23,224 kg (51,200 lb)
Minimum operating empty weight: 21,772 kg (48,000 lb)
NOTE
The maximum take-off weight (MTOW) and/or maximum landing
weight (MLW) may be further limited due to performance
considerations.
B. Buoyancy Limitations
(1) TAKE-OFF ON RUNWAYS NEAR BODIES OF WATER
• For take-off at weights above the maximum landing weight, OUTFLOW VLV 2 must
be closed and one air-conditioning pack must be shutdown for take-off.
(2) LANDING ON RUNWAYS NEAR BODIES OF WATER
• For forced / emergency landing at weights above the maximum landing weight,
OUTFLOW VLV 2 must be closed and one air-conditioning pack must be shutdown
for landing.
LIMITATIONS
STRUCTURAL WEIGHT
REV 13, Nov 10, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−02−1
LIMITATIONS
STRUCTURAL WEIGHT
Flight Crew Operating Manual Mar 12, 2004
CSP 700−5000−6
Volume 1
02−02−2
THIS PAGE INTENTIONALLY LEFT BLANK
1. CENTRE OF GRAVITY
A. Centre Of Gravity Limits
The maximum permissible centre of gravity (CG) limits are as shown in Figure 02−03−1.
The airplane including interior payload, passengers and fuel must be loaded such that the
airplane weight and centre of gravity are maintained within the specified limits (including any
variation due to fuel consumption, passenger movement, retraction of landing gear, etc. ).
The airplane must be loaded in accordance with the loading instructions associated with the
Weight and Balance Manual (BD 700−1A11−WBM).
LIMITATIONS
CENTRE OF GRAVITY
Mar 12, 2004 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−03−1
1. CENTRE OF GRAVITY (CONT'D)
A. Centre Of Gravity Limits (Cont’d)
GF0203_005
LIMITATIONS
CENTRE OF GRAVITY
Centre of Gravity (CG) Envelope
Figure 02−03−1
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